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contributor authorJ. B. McVey
contributor authorJ. B. Kennedy
contributor authorS. Russell
date accessioned2017-05-08T23:30:03Z
date available2017-05-08T23:30:03Z
date copyrightJanuary, 1989
date issued1989
identifier issn1528-8919
identifier otherJETPEZ-26662#53_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/105428
description abstractExperimental data on the characteristics of the spray produced by a gas turbine engine airblast fuel injector are reported. The data acquired include the mass-flux distribution, measured by use of a high-resolution spray patternator; the gas-phase velocity field, measured by use of a two-component laser-Doppler velocimeter; and the liquid droplet size and velocity distributions, measured by use of a single-component phase-Doppler anemometer. The data are intended for use in assessments of two-phase flow computational methods as applied to combustor design procedures.
publisherThe American Society of Mechanical Engineers (ASME)
titleApplication of Advanced Diagnostics to Airblast Injector Flows
typeJournal Paper
journal volume111
journal issue1
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3240227
journal fristpage53
journal lastpage62
identifier eissn0742-4795
keywordsFlow (Dynamics)
keywordsLasers
keywordsVelocimeters
keywordsResolution (Optics)
keywordsCombustion chambers
keywordsDesign
keywordsEjectors
keywordsGas turbines
keywordsSprays
keywordsTwo-phase flow
keywordsFuel injectors AND Computational methods
treeJournal of Engineering for Gas Turbines and Power:;1989:;volume( 111 ):;issue: 001
contenttypeFulltext


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